Heat treatment for alloys particularly steels to be used in sour well service

ABSTRACT

Steel characterized by high yield strength, e.g., over 90,000 p.s.i., is rendered greatly less susceptible to Sulfide Corrosion Cracking in sour oil wells or comparable environments through the use of a sequence of heat treating operations in which the steel is heated within its Ac1 and Ac3 region and thereafter heated below its Ac1 temperature.

United States Patent Shape et a1.

1 1 Apr. 11, 1972 [54] HEAT TREATMENT FOR ALLOYS PARTICULARLY STEELS TO BE USED IN SOUR WELL SERVICE [72] Inventors: Edwin Snape, Monsey, N.Y.; Frank W.

Schaller, Ringwood Passaic, NJ.

The International Nickel Company, Inc., New York, NY.

[221 Filed: Mar. 10,1969

211 Appl.No.: 805,827

[73] Assignee:

52 u.s.c1 ..148/134,148/3l,148/36, 148/37,148/135,148/142,l48/143,148/144 51 1111.01. ..C21dl/18 [58] FieldofSearch ..l48/142,143,134,144,36, 148/31,135,37

[5 6] References Cited UNITED STATES PATENTS 2,097,878 11/1937 Grabe ..l48/l43 2,664,369 12/1953 Kiefer 148/1 34 3,288,657 11/1966 Morita et al. ..148/143 3,370,994 2/1968 Konkol 148/ l 34 Primary Examiner-Richard 0. Dean Attorney-Maurice L. Pinel [57] ABSTRACT 26 Claims, No Drawings HEAT TREATMENT FOR ALLOYS PARTICULARLY STEELS TO BE USED IN SOUR WELL SERVICE As those skilled in the art are well aware, the petroleum industry has, for close to years, been confronted with a perplexing problem commonly referred to as Sulfide Corrosion Cracking, a problem of no little magnitude. In point of historical origin, the dilemma seemingly first manifested itself (doubtless there were others) circa 1950 in connection with the unexpected failures of oil well tubing in sour oil wells located in Canada, the failures being unexpected to the extent that the steel from which the tubing was fabricated had given excellent service prior thereto, though, it appears, in sweet condensate wells. In any event, since that time investigations into the causes of such failures have been many, and extensive as well as intensive. And there have been a number of solutions advanced, many of which have been deemed impractical by reason of economic considerations while others have imposed such severe commercial limitations as to be unsuitable.

All the research notwithstanding, there ostensibly is not yet an unanimously accepted theory as to the mechanism responsible for Sulfide Corrosion Cracking. But there is a considerable body of authoritative opinion which reflects that both hydrogen embrittlement and stress corrosion cracking phenomena are involved. And there does seem to be virtual accord that steels of high yield strength, particularly above 90,000 pounds per square inch (psi), are exceptionally prone to Sulfide Corrosion Cracking. Too, it might be added that cracking of the type under consideration appears to be relatively spontaneous in occurrence, thus rendering detecting devices of doubtful value. This, of course, only accentuates the gravity of the difficulty, which has been expressed in terms that if either the casing or tubing in a high pressure sour well should fail, apart from other damage, the well itself might be lost.

As to the nature of the problem itself and assuming both hydrogen and stress to be involved, it has been considered that hydrogen in nascent form first penetrates the steel surface, steel exhibiting a rather striking affinity for hydrogen. The initial point of hydrogen entry seems concentrated at such sites as voids, discontinuities, inclusions, or other points of imperfection. In sour oil and/or gas wells and apart from other sources, the hydrogen can be introduced by corrosive attack of the steel (tubing, casing, etc.). Regardless of the source, the supply of atomic hydrogen is unfortunately ample.

It has been postulated that upon penetration of the steel surface, the nascent or atomic hydrogen tends to accumulate and form molecular hydrogen. This in turn is thought to bring about a volume expansion of hydrogen in the void, etc. Thus, a stress pattern is set up (the hydrogen aspect of the problem) which together with internally and externally induced pressures (the stress cracking part) causes the formation or extension of a crack which with time continues to propagate under pressure until failure.

As a practical matter, it is virtually impossible to prevent the occurrence of either internal or external stresses. For example, it is conventional to cold work tubing and the like simply to straighten the same and cold work is a classical method of inducing internal stress. Similarly, certain heat treatments are conducive to internal stressing, quenching from austenitizing being a prime example. As to external pressures, the weight of equipment and gas pressures are exemplary.

Accordingly, it has been proposed to use various inhibitors, coatings (prevent hydrogen penetration), liners (of special alloys to allow for permeation of the liner by atomic hydrogen such that the hydrogen transforms into the molecular state which is passive to steel), and different metals such as stainless steels and nickel-base alloys (proposals considered too expensive). None of these solutions, which are but illustrative, seem to have attained a point of acceptance at least with regard to steels having yield strengths above 90,000 psi.

Therefore, there has been a distinct commercial need for low cost steel characterized by high yield strength e. g., 90,000 psi or more, which greatly resists Sulfide Corrosion Cracking.

The emphasis is on yield strength as well as resistance to cracking because such strength levels are most desirable for the deeper sour wells since the external pressures are greater. Of course, as mentioned herein, it has been the higher strength steels which have proven to be the most susceptible to attack. For this reason the National Association of Corrosion Engineers (NACE) recommended that steels to be used in sour wells be tempered such that the yield strength thereof not exceed 90,000 psi, and the American Petroleum Institute (API) introduced a specification to this effect in 1963. Insofar as we are aware, this remains the practice currently prevailing, a point seemingly confirmed by a recent article which indicated that at yield strengths above 100,000 psi no known alloy except a certain copper-nickel alloy completely resists the onset and failure by way of Sulfide Corrosion Cracking. All steels failed. It is to this problem which the present invention is primarily addressed.

It has now been discovered that the capability of steels characterized by high yield strengths, 90,000 psi and above, e.g., 100,000 psi, to resist Sulfide Corrosion Cracking are markedly enhanced provided the steels are subjected to a special sequence of heat treating operations as described herein.

It is an object of the invention to provide steels of yield strengths on the order of 90,000 psi and higher which, despite their strength, display a greatly improved ability to resist the degradation effects of Sulfide Corrosion Cracking.

Other objects and advantages of the invention will become more apparent from the following description.

Generally speaking, the present invention contemplates subjecting a steel to a two-stage heat treatment in which the steel is first brought to a temperature within its A, and A region (often referred to herein as the intercritical temperature), cooled, and thereafter again heated but to a temperature below its A the steel again being cooled. (It is to be understood, of course, the first stage heat treatment can be preceded by other treatments including such conventional treatments as normalizing or austenitizing and quenching.)

Upon heating above the A temperature, a phase change takes place in which a portion of the metal structure is converted into austenite which upon cooling transforms whereby a metal matrix is formed containing a decomposition production of austenite. This decomposition product, for example, martensite, should not constitute more than about 50 percent, by volume, of the metal matrix. For, in carrying the invention into practice, should the first stage temperature be too high, the microstructure upon cooling therefrom is one obtained in which the matrix is predominantly influenced by the austenite decomposition product, e.g., martensite, and it has been found, as will be illustrated herein, that in such instances the steel can be rendered susceptible to Sulfide Corrosion Cracking. Accordingly, it is advantageous that the intercritical temperature be controlled such that not more than about 30 percent or 40 percent of the austenite decomposition product is formed upon cooling therefrom. (Of course, the exact intercritical temperature will vary from steel to steel since, as is well known to those skilled in the art, A temperature (also A depends upon composition. However, it is merely a routine matter to determine the point at which, for example, more than about 50 percent martensite forms for any given composition.) On the other hand, the intercritical temperature should be sufficiently high, i.e., above the A temperature, so as to provide a microstructure containing at least about 5 percent, and beneficially at least 10 percent, of the decomposition product upon cooling.

With regard to the duration a steel should be held within its A A temperature range, long holding periods should be avoided since they only add to cost. A suitable period would be up to 4 hours, e.g., 15 minutes to 2 hours. Cooling from the A A temperature should be carried down past the temperature necessary to transform the austenite, for example, below the M, and preferably below M, temperature in the case of martensite. Other operations can be carried out to effect maximum transformation, e.g., cold treating as by refrigeration down to below, say- F.

Concerning the second stage treatment, the temperature used, of course, should not exceed the A lest the first stage be simply repeated. Preferably, the temperature should be at least 25 F. or 50 F. below A a range of 50 F. to 300 F. below A being suitable. However, for nickel steels, particularly high nickel steels, e.g., 5 percent or more, a temperature of at least 100 F. below, and preferably at least 200 F. below, A should be used. Cooling can be conducted by air, oil quenching, water quenching, etc. (This also applies to cooling from the intercritical temperature.)

While the exact mechanism which might explain the theory involved is not yet completely at hand, the effect of the abovedescribed two-stage heat treatment might be considered unusual. To simply double temper a steel below its A temperature does not result in any significant improvement in respect of Sulfide Corrosion Cracking (failure obtains). Moreover, conventional double tempering at best usually results in a loss of strength accompanied by a slight increase in toughness. This focuses attention upon heat treating between the A and A temperatures. From what has heretofore appeared in the literature, it would seem that such a heat treatment should not be employed. To explain it has been previously said that the formation of martensite is an excellent way to actually promote Sulfide Corrosion Cracking. However, the intercritical treatment contemplated herein encompasses the intentional formation of martensite. But when the matrix so formed is tempered below the A temperature, what might otherwise have been a crack-prone steel becomes a steel greatly resistant to sulfide corrosion cracking.

Actually, it has been found that in respect of certain steels the dual step heat treatment in accordance herewith contributes to higher strength levels notwithstanding the fact that the second heating is a tempering treatment in which a loss in strength and an increase in ductility would be expected. The increase in ductility is readily understandable since hard austenite decomposition products, such as martensite, formed upon cooling from the intercritical temperature are softened by tempering. More difficult to explain, however, is the simultaneous increase in strength. In any case, it is considered that the mechanism involves stress-strain behavior. It has been noted that in single tempering below the A temperature of such steels, a sharp yield point is observed which disappears as the temperature is raised to just above A yield strength also decreasing. A further increase in temperature above A but well below A results in a substantial strength increase; however, the yield point does not reappear. This behavior indicates a straining of the matrix by transformation of the austenite region. Thereupon, tempering below A enables strain aging to occur in the plastically deformed regions of the matrix and restores the yield point whereby strength is increased. (This overall behavior is often referred to herein as intercritical strengthening".

lntercritical strengthening occurs particularly in respect of nickel-containing steels, and more particularly as to those steels which also contain at least one temper resistant element such as molybdenum, chromium, silicon, vanadium, tungsten, etc. The nickel content can be as high as percent although a range of from 1 to 5 or 7.5 percent is satisfactory. Up to 3% molybdenum, up to 4% chromium, up to 3% silicon, up to 3% vanadium, up to 1% carbon (and preferably at least 0.2% carbon) as well as other desired constituents can be present in the steels. Such other constituents include age hardening constituents such as copper, aluminum and titanium in the following percentages: up to 3% copper, up to 2% aluminum and up to 2% titanium. Further, columbium and boron may be present in amounts up to 2% and up to 0.25%, respectively. A steel containing from 1 to 10% nickel and at least one or more temper resistant constituents in the following ranges is deemed suitable: 0.05 to 2% molybdenum, 0.5 to 3% chromium, 0.2 to 1% silicon, 0.1 to 1% vanadium, 0.1 to 0.5% carbon, 0.05 to 2% tungsten, the balance being essentially iron. A particularly satisfactory steel contains from 0.3 to 0.5% carbon, from 0.4 to 1% manganese, from 1.25 to 2.5% nickel, 0.4 to 1.25% chromium, 0.1 to 0.75% molybdenum. Another illustrative steel contains about 0.05 to 0.2% carbon, from 1.75 to 2.75% chromium, from 0.5 to 1.5% molybdenum. As contemplated herein, the nickel content can be replaced in whole or in part by an equivalent amount of manganese. Moreover, it is considered that the subject invention could be used in connection with certain stainless steels containing from about 1 l to 14 percent chromium.

In order to give those skilled in the art a better understanding of the invention the following illustrative data are given.

A series of commercially produced steels, C-75, AISI M40 .and AlSI 4340, the composition of which are given in Table l, were heat treated in accordance with the invention and, for purposes of comparison, by other heat treatments, the heat treatments being set forth in Table II. Alloy C was an open hearth heat from which 2 /8 inch O.D. tubing had been formed. Specimens were longitudinally cut therefrom for test. The AlSl steels 4140 and 4340, which had been produced using an electric furnace, were hot rolled from 1 l/8 inch round bar stock and 4 4 inch squares, respectively, to inch plate from which specimen blanks were cut.

After testing for mechanical properties, (results reported in Table II) specimens were finished machined to a dimension of approximately 3X A X is inch. Notch beam specimens were then made, the notch being cut transversely to the direction of hot rolling with an included angle of 45 and a notch radius of 0.010 inch. Two specimens for each condition of heat treatment were deflected to the yield deflection in three-point loaded fixtures, a common testing procedure. The deflection necessary to approximately reach the onset of plastic deformation was determined using instrumented bend tests.

The loaded specimens were then immersed in a 5-liter flask containing an aqueous solution of 5% NaCl and 0.5% acetic acid, nitrogen being passed through the solution for about 30 minutes to purge the system of oxygen. The solution was then saturated with H 5 which was continuously bubbled therethrough. Prior to opening the flask for examination of the specimens, the nitrogen purge was again repeated. Inspections were carried out after the second and seventh days and every seven days thereafter (as to uncracked specimens) until a predesignated period of thirty days (total) elapsed, after which the test was discontinued. To avoid accumulation of corrosion products (which might have otherwise interfered with accuracy of the results) and to also keep the pH constant at about 3.8, the solution was changed after each inspection. In various instances threshold stress values were determined, i.e. threshold values at or below yield deflection. With respect to specimens which exhibited early failure, the threshold evaluation was one of reducing the percent of yield deflection to successively lower levels until a stress level was reached (2 5000 psi) at which no failure occurred within an exposure period of 30 days.

TABLE I.CHEMICAL COMPOSITION C, Mn, Si, Ni, Cr, Mo, A1, P, S, Fe, Alloy percent percent percent percent percent percent percent percent percent percent 0. 47 1.47 n.d. n.d. 0. 04 0.21 n.d. n.d. n.d. Bal. 0. 38 0.79 O. 34 0. 15 l. 01 0. 17 n.d. 0. (I09 0. 027 Bal. 0. 44 0.71 0. 28 1.82 0. 79 0. 25 0. 025 0. 008 0.01 Bal.

n.d. Not determined.

Bel. =Balance iron plus impurities.

TABLE II Specimen Yield Yield failures Threshold Heat treatment point, stress, Elon., R.A.. stress, hours at F. p.s.i. p.s.i. percent percent percent Days p.s.i

Alloy:

C45 1 1 1 1 1 1 1 1/1600, W.Q 1 1 1 1 1 1 1 1 1 1 1 1 95, 700 23. 6 61. 5 100 2 tLd.

Plus 1/1,325, A.C 1 1 1 1 99,300 20.0 63.0 1 1 1 1 1 1 n. l.

C-75 1 1 1 1 1 1/1,600, W.Q 88,500 83,600 25.5 62.0 1 1 1 1 1 1.

Plus 1/1,325, A.C 90,200 83,600 1 1 1 1 1 1 1 1 1 1 1 Plus l/1,200, AC 1 1 1 1 1 1 1 1 1 1 1 1 1 1 C-75 1 1/1,600, W.Q 1 1 1 110, 300 20. 0 60. 0 100 2 50, 000

Plus 1/1,350, A.C 1 1 1 1 1 1 1 1 100, 300 20.0 61.0 1 1 1 1 1 1 1 1 1 C-75 1 1 1 1 1 1 1 1/1,600, W.Q 1 1 1 1 1 1 1 1 96, 400 89, 400 25. 4 64. 5 0

Plus 1/1,350, A.C 98, 600 89,200 23. 6 64. 0 Plus 1/1,100, A.C

AISI4140 1/1,650, O.Q 78,200 21.0 44. 0 100 2 Plus 1/1,400, A.C 1 1 1 1 1 1 1 78, 200 21.0 50.0 1.

AISI4140 1/1,650, O,Q 1 1 88,200 84, 200 26.0 66. 5 0 88, 500 Plus 1/1,350, A.C 88,700 84, 700 26.0 66. 5 Plus 1/1,100, A.C

AISI4340 1/1,650, O.Q 124, 600 123,000 22. 0 66. 0 100 8-14 n.0-

Plus 1/1,200, A.C 124, 000 123, 400 22. 0 67.0

AISI4340 1 1 1 1 1/1,650, O.Q 1 106, 200 97, 800 24. O 53. 5 50 3- 500 Plus 1/1,250, A.C 1 108,800 98, 400 25.0 54. 0

AISI434O 1 1 1/1,650, O.Q 91, 800 24. 0 55. 5 100 2 000 Plus 1/1,325, AC 1 93,000 23.0 54. 0

AISI-1340 1/1,650, O.Q 1 103, 600 97,800 25.0 66. 5 Plus 1/1,325, A.C 111,600 98, 200 25. 0 69.0 Plus 1/1,100, A.C 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1.

AISI4340 1 1,s50, O.Q 1. 95, 200 21.0 52. 5 100 2 000 Plus 1,350, 11.0 .1 95,000

AISI4340 1/1,650, O.Q 107,200 112, 400 Plus 1/1,350, A.C 107, 300 112, 400 Plus 1/1,100, A.C

AISI4340 1 1/1,650, O.Q 1 102, 800' 12.0 28.0 100 2 Plus 1/1,375, A.C 97, 200

Plus 1/1,375, A.C 115, 800 112, 400 25.0 67. 5

Plus 1/1,100, A.C 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 n.d.=not determined; W.Q.=Water Quenched; A.C.=Air Cooled; O.Q.=Oil QuenchedApproximate Au and A53 temp 0-75. 1,301 F. and 1,501? for 1181 4140,, 15512114291 g 1, 59 111"; ior AISI 4340, 1,251 F.V1,275 F. and 1 ,101 EX-1,451 F.

In perusing the data given in Tables I and II it will be observed that in each instance in which a steel specimen was treated in accordance with the invention complete resistance to Sulfide Corrosion Cracking obtained over the full day period of test. This is in marked contrast to the failure characteristic of all specimens treated in a manner beyond the scope of the invention (but not inconsistent with conventional practice). It should also be particularly noted that in many instances the yield strength (yield point or yield stress) exceeded 100,000 psi and yet Sulfide Corrosion Cracking did not occur. This is thought to be quite significant inasmuch as the testing procedure used is considered to be one of considerable severity. Note should be taken of the AISI 4340 specimens heated to the intercritical temperature of 1,375 F. While this temperature is below the A for the steel, nonetheless, it represents a situation referred to above herein in which the amount of martensite formed upon cooling from the l,375 F. temperature was excessive (above 50 percent) such that upon subsequent tempering Sulfide Corrosion Cracking resulted. A most desirable microstructure as contemplated herein consists of a ferritic matrix containing relatively uniformly distributed carbide particles and tempered martensite.

With particular regard to AISI 4340, a steel which contained nickel together with such temper resistant constituents as molybdenum and chromium, the yield strength actually increased upon the second stage (tempering) treatment. This is reflected by the data concerning the intercritical temperature of 1,350 F., the yield stress being raised by a value of about 7,000 psi. Normally, as indicated previously a loss in strength would be expected as a result of the tempering (softening) treatment below A Together with the increase in strength, ductility was also considerably improved as can be seen from a comparison of the tensile elongation (Elong., percent) and reduction in area (R.A., percent) figures.

This result whereby strength is improved by a tempering treatment, or is not impaired but toughness is considerably enhanced, is also reflected by the data given in connection with the steels set forth in Tables III and IV.

TABLE III.CHEMICAL COMPOSITION n.a. not added. n.d. =not determined. Ba1.=balance ironplus impurities (phosphorus, su ll'ug e tcl W "W TABLE IV C.V.N., 0.2% Offset U.T.S., Elong., R.A., It.-lbs. Heat Treatment Y.S., p.s.i. p.s.l. percent percent (-320 F.)

85,00095,000 25 plus 1/1050, A.C. plus 1/000, A.C 110,000 11 i, 000 22 78. 23 plus 1/1100, A.C. plus 1/600, 11.0... 105, 800 111,200 23 78 58 plus 1/1150, 11.0. plus 1/600, A.C 97,200 105,100 24 80 129 plus 1/1250, A.C. plus 1/000, A.C 97, 200 112,000 78 120 plus 1/1350, A.C. plus 1/600, AC. 119, 000 129,000 17 77 115 37 plus 1/1150, A.C. plus 1/950, A.C 108,600 113,400 23 74. 5 20 plus 1/1150, A.C. plus 1/600, A C 107, 600 112,200 23 76 54.5 plus 1/1150, 11.0. plus 1/950, A C... 09,400 130,700 26 64. 5 28 plus 1/1150, A.C. plus 1/600, A.C. 90, 400 130, 900 28 68 44 plus 1/1100, A.C 98, 000 105,200 73, 5 28 50, Plus l/1100, A.C. plus 1/850, A.C. 130,000 133,900 0, plus 1/1200, AC. plus 1/850, AC.-. 113,300 124, 500 21 70 36 plus 1/1300, A.C 62, 700 116, 800 25 55. 5 l 3. 0 1/1600, W.Q. plus 1/1300, A.C. plus 1/800, A.C 82, 000 93, 600 29 71 1 55 1 Cut in diflerent direction and tested at 200 F. 9 eaflaLQPfZ; ar e-.1.

Apart from the strength and/or toughness being improved, in connection with the steels set forth in Tables Ill and 1V it should be particularly mentioned that with regard to the series of the 9 percent nickel steel the results were significantly better when the second stage heat treatment was conducted more than 100 F. below the A, temperature. (The A temperatures for Alloys 9 Ni-A, 9 NiB and 9 Ni-C are on the order of 1050 F., 1025 F. and 1000 F., respectively.)

While the invention as described above has been primarily directed to resisting Sulfide Corrosion Cracking in steels of yield strengths of 90,000 psi or above, it is to be understood, of course, that steels of lower yield strength can be treated in accordance herewith. However, to minimize the possibility of Sulfide Corrosion Cracking, it is preferred to use a steel in which the yield strength is less than 120,000 psi. Castings may be given the double stage heat treatment as well as wrought products. In this regard, it is contemplated that cast irons may also be so treated in which case the carbon content can be as high as 4 or 5 percent together with the conventional elements commonly found in cast irons, e.g., nickel, manganese, chromium, molybdenum, vanadium, etc.

Although the present invention has been described in conjunction with preferred embodiments, it is to be understood that modifications and variations may be resorted to without departing from the spirit and scope of the invention, as those skilled in the art will readily understand. Such modifications and variations are considered to be within the purview and scope of the invention and appended claims.

We claim:

1. A process for improving the resistance of steel to sulfide corrosion cracking which comprises bringing into contact with a sulfide corrosion cracking environment a steel which has been, (a) heated above its A temperature but below its A temperature to effect a phase change in which part of the metal structure transforms to austenite, the temperature being controlled such that upon cooling not more than about 50 percent of an austenite decomposition product is formed, (b) cooled such that a metal matrix is formed containing the decomposition product of austenite, (c) heated to a temperature below its A temperature, and (d) thereafter cooled to form a metal matrix containing relatively uniformly distributed carbide particles and a tempered decomposition product of austenite.

2. A process in accordance with claim 1 in which the steel upon cooling from the second stage heating has a yield strength of at least about 90,000 psi.

3. A process in accordance with claim 2 in which the yield strength of the steel is less than 120,000 psi.

4. A process in accordance with claim I in which the amount of austenite decomposition product formed is at least about 5 percent and the second stage heat treatment is conducted more than 100 F. below the A temperature.

5. A process in accordance with claim 1 in which the amount of austenite decomposition formed is not more than about 40 percent and the second stage heat treatment is conducted more than 100 F. below the A temperature.

6. A process in accordance with claim 4 in which the amount of decomposition formed is not more than about 30 percent and the second stage heat treatment is conducted more than 200 F. below the A temperature.

7. A process in accordance with claim 1 in which nickel is present in an amount up to about 10 percent,

8. A process In accordance with claim 1 in WlllCl'l the steel contains at least one temper-resistant constituent in the following ranges: up to 3% molybdenum, up to 4% chromium, up to 3% silicon, up to 3% vanadium and up to 3% tungsten.

9. A process in accordance with claim 7 in which the nickel is from 1 to 7.5 percent.

10. A process in accordance with claim 8 in which the steel contains at least one temper-resistant element in the following ranges: 0.05 to 2% molybdenum, 0.5 to 3% chromium, 0.2 to 1% silicon, 0.1 to 1% vanadium and 0.05 to 2% tungsten.

11. A process in accordance with claim 7 in which the steel contains carbon in an amount of at least 0.2 percent.

12. A process in accordance with claim 8 in which the steel contains carbon in an amount of at least 0.2 percent.

13. A process in accordance with claim 1 in which the steel contains about 0.3 to 0.5% carbon, about 0.4 to 1% manganese, about 1.25 to 2.5% nickel, about 0.4 to 1.25% chromium and about 0.1 to 0.75% molybdenum.

14. A process in accordance with claim 1 in which the steel contains about 0.05 to 0.2 percent carbon, about 1.75 to 2.75% chromium and about 0.5 to 1.2% molybdenum.

15. A process in accordance with claim 1 in which the decomposition product of austenite is substantially martensite.

16. A process in accordance with claim 5 in which the austenite decomposition product is substantially martensite.

17. A process in accordance with claim 7 in which the austenite decomposition product is substantially martensite.

18. A process in accordance with claim 8 in which the austenite decomposition product is substantially martensite.

19. A process in accordance with claim 15 in which the microstructure obtained upon cooling from below the A temperature consists of a ferritic matrix containing relatively uniformly distributed carbide particles and tempered martensite.

20. A process in accordance with claim 16 in which the microstructure obtained upon cooling from below the A temperature consists of a ferritic matrix containing relatively uniformly distributed carbide particles and tempered martensite.

21. A process in accordance with claim 17 in which the microstructure obtained upon cooling from below the A temperature consists of a ferritic matrix containing relatively uniformly distributed carbide particles and tempered martensite.

22. A process in accordance with claim 18 in which the microstructure obtained upon cooling from below the A temperature consists of a ferritic matrix containing relatively uniformly distributed carbide particles and tempered martensite.

23. A process in accordance with claim 7 in which the second stage heat treatment is conducted more than 100 F. below the A temperature when the steel contains at least 5 percent nickel.

24. A process in accordance with claim 9 in which the second stage heat treatment is conducted more than l F.

below the A temperature when the steel contains at least percent nickel.

P0405) UNITED STATES PATENT OFFICE QE'HFKCATE E 2'; EQTION Patent No. 3655465 naged Aprll 11, 1972 Inventer (a) EDWIN SNAPE and FRANK W SCI-IALL'ER It is certified that error appears in the above-identified patent and that said Letters Patent are hereby corrected as shown below:

Table 11, Yield point, p.s.i. line 23, for "111,600" read "101,600";

Yield stress, p.'s.i. line 6, for 110,300" read "100,300";

Yield stress, p.s.i. lines 27 & 28, for "112,400" read 102,400"

Table II notation, second line,

for C-'75,1,? 01F. and 1,401F.; for A151 4140, 1,351F.1,401F.

and 1,501F.; for A151 4340, 1,251F.-l,275F. and 1,401F .,1,451F."

read "C-75, 1,300F. and 1,400F.; for A151 4140, 1,35(?F.l400F.

and 1,500F.; for A151 4340, 1250F.-1,275F. and 1,400F.1,450F."

Claim 1, lines 2 and 4, delete quotations.

Signed and sealed this 22nd day of January 197L (SEAL) Attest:

EDWARD M.FLETCHER,JR. RENE D. TEGTMEYER Attesting Officer Acting Commissioner of Patents 

2. A process in accordance with claim 1 in which the steel upon cooling from the second stage heating has a yield strength of at least about 90,000 psi.
 3. A process in accordance with claim 2 in which the yield strength of the steel is less than 120,000 psi.
 4. A process in accordance with claim 1 in which the amount of austenite decomposition product formed is at least about 5 percent and the second stage heat treatment is conducted more than 100* F. below the Ac1 temperature.
 5. A process in accordance with claim 1 in which the amount of austenite decomposition formed is not more than about 40 percent and the second stage heat treatment is conducted more than 100* F. below the Ac1 tempeRature.
 6. A process in accordance with claim 4 in which the amount of decomposition formed is not more than about 30 percent and the second stage heat treatment is conducted more than 200* F. below the Ac1 temperature.
 7. A process in accordance with claim 1 in which nickel is present in an amount up to about 10 percent.
 8. A process in accordance with claim 1 in which the steel contains at least one temper-resistant constituent in the following ranges: up to 3% molybdenum, up to 4% chromium, up to 3% silicon, up to 3% vanadium and up to 3% tungsten.
 9. A process in accordance with claim 7 in which the nickel is from 1 to 7.5 percent.
 10. A process in accordance with claim 8 in which the steel contains at least one temper-resistant element in the following ranges: 0.05 to 2% molybdenum, 0.5 to 3% chromium, 0.2 to 1% silicon, 0.1 to 1% vanadium and 0.05 to 2% tungsten.
 11. A process in accordance with claim 7 in which the steel contains carbon in an amount of at least 0.2 percent.
 12. A process in accordance with claim 8 in which the steel contains carbon in an amount of at least 0.2 percent.
 13. A process in accordance with claim 1 in which the steel contains about 0.3 to 0.5% carbon, about 0.4 to 1% manganese, about 1.25 to 2.5% nickel, about 0.4 to 1.25% chromium and about 0.1 to 0.75% molybdenum.
 14. A process in accordance with claim 1 in which the steel contains about 0.05 to 0.2 percent carbon, about 1.75 to 2.75% chromium and about 0.5 to 1.2% molybdenum.
 15. A process in accordance with claim 1 in which the decomposition product of austenite is substantially martensite.
 16. A process in accordance with claim 5 in which the austenite decomposition product is substantially martensite.
 17. A process in accordance with claim 7 in which the austenite decomposition product is substantially martensite.
 18. A process in accordance with claim 8 in which the austenite decomposition product is substantially martensite.
 19. A process in accordance with claim 15 in which the microstructure obtained upon cooling from below the Ac1 temperature consists of a ferritic matrix containing relatively uniformly distributed carbide particles and tempered martensite.
 20. A process in accordance with claim 16 in which the microstructure obtained upon cooling from below the Ac1 temperature consists of a ferritic matrix containing relatively uniformly distributed carbide particles and tempered martensite.
 21. A process in accordance with claim 17 in which the microstructure obtained upon cooling from below the Ac1 temperature consists of a ferritic matrix containing relatively uniformly distributed carbide particles and tempered martensite.
 22. A process in accordance with claim 18 in which the microstructure obtained upon cooling from below the Ac1 temperature consists of a ferritic matrix containing relatively uniformly distributed carbide particles and tempered martensite.
 23. A process in accordance with claim 7 in which the second stage heat treatment is conducted more than 100* F. below the Ac1 temperature when the steel contains at least 5 percent nickel.
 24. A process in accordance with claim 9 in which the second stage heat treatment is conducted more than 100* F. below the Ac1 temperature when the steel contains at least 5 percent nickel.
 25. A process in accordance with claim 17 in which the second stage heat treatment is conducted more than 100* F. below the Ac1 temperature when the steel contains at least 5 percent nickel.
 26. A process in accordance with claim 11 in which the steel contains about 1 to about 10 percent nickel. 